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    Pressure regulator and method of using the same
    4.
    发明授权
    Pressure regulator and method of using the same 有权

    公开(公告)号：US12146687B2

    公开(公告)日：2024-11-19

    申请号：US16787554

    申请日：2020-02-11

    Applicant: GOODRICH CORPORATION

    Inventor： Yasasvi Harish Kumar ,  Skandan Berikai Kuppan ,  Satya Swaroop Panda

    IPC: G05D16/02 ,  C01C1/04 ,  F24V30/00 ,  G05D16/00

    Abstract: Disclosed is a pressure regulator, comprising: a first cylindrical chamber; a second cylindrical chamber located concentrically within the first cylindrical chamber and in thermal communication with the first cylindrical chamber; and further comprising at least one of: an internal valve, wherein the internal valve is connected at a first end to the first cylindrical chamber and at a second end to the second cylindrical chamber, wherein the internal valve allows the flow of gas from the second cylindrical chamber to the first cylindrical chamber; and an external gas chamber and an external valve, wherein the external gas chamber is located outside the first cylindrical chamber, wherein the external valve is connected at a first end to the first cylindrical chamber and at a second end to the external gas chamber, wherein the external valve allows the flow of gas from the external gas chamber to the first cylindrical chamber.

    Aircraft egress system
    6.
    发明授权
    Aircraft egress system 有权

    公开(公告)号：US12151824B2

    公开(公告)日：2024-11-26

    申请号：US17152952

    申请日：2021-01-20

    Applicant: Goodrich Corporation

    Inventor： Skandan Berikai Kuppan ,  Jeffrey Martin Werbelow ,  Satya Swaroop Panda

    IPC: B64D25/14 ,  F04D17/10 ,  F04D25/06 ,  F04D27/00 ,  F04D29/42

    Abstract: Disclosed is an egress pack for egressing a craft. The egress pack includes an egress aid defining a cavity and an inflation port. The egress pack includes an inflation duct connected with the inflation port for supplying gas to the cavity. The inflation duct defines a flow direction oriented to supply the cavity. The inflation duct defines a first ingress port defined by a first boundary and defining a primary flow path in the flow direction. The inflation duct defines a second ingress port defining a secondary flow path in fluid communication with the primary flow path. The inflation duct defines a divider disposed between the first ingress port and the second ingress port that coincides with the first boundary.

    AIRCRAFT EGRESS SYSTEM
    7.
    发明申请
    AIRCRAFT EGRESS SYSTEM 有权

    公开(公告)号：US20210229820A1

    公开(公告)日：2021-07-29

    申请号：US17152952

    申请日：2021-01-20

    Applicant: Goodrich Corporation

    Inventor： Skandan Berikai Kuppan ,  Jeffrey Martin Werbelow ,  Satya Swaroop Panda

    IPC: B64D25/14 ,  F04D25/06 ,  F04D17/10 ,  F04D27/00 ,  F04D29/42

    Abstract: Disclosed is an egress pack for egressing a craft. The egress pack includes an egress aid defining a cavity and an inflation port. The egress pack includes an inflation duct connected with the inflation port for supplying gas to the cavity. The inflation duct defines a flow direction oriented to supply the cavity. The inflation duct defines a first ingress port defined by a first boundary and defining a primary flow path in the flow direction. The inflation duct defines a second ingress port defining a secondary flow path in fluid communication with the primary flow path. The inflation duct defines a divider disposed between the first ingress port and the second ingress port that coincides with the first boundary.

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